High temperature rolling element bearing
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorsLewis Rosado, Nelson H. Forster, Wei T. Shih
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AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorsLewis Rosado, Nelson H. Forster, Wei T. Shih
Estimating the term…
A novel rolling element bearing assembly comprises an inner race, an outer race, a plurality of rolling elements, and a carbon-carbon composite retainer. The carbon-carbon composite retainer is fabricated by providing a woven tube, cutting the woven tube into suitably sized rings, piercing the rings for rolling bearing elements, and densifying the resulting retainer. Alternatively, the tube can be densified, then cut into a plurality of retainer blanks which are then pierced. For use at operating temperatures above about 650.degree. C., ceramic coatings, such as silicon carbide (SiC), silicon nitride (Si.sub.3 N.sub.4) and boron nitride (BN) can be used to provide oxidation resistance for the carbon-carbon composite retainer at such elevated temperatures.
A rolling element bearing assembly comprising an inner race, an outer race, a plurality of rolling elements, and a carbon-carbon composite retainer wherein said composite retainer is coated with a ceramic coating.
A rolling element bearing assembly comprising an inner race, an outer race, a plurality of rolling elements, and a carbon-carbon composite retainer wherein said retainer is coated with a phosphorous-containing compound.
Dependencies are inferred from the claim text.